| astronautix.com | August 19 |
1920 - Nation: USA.
Final test of cartridge rocket (a series of smokeless power cartridges, automatically loaded into a gun barrel and fired in sequence to produce thrust). Four of the five cartridges fire, but the fifth jams. The rocket only achieves 60 feet, the highest altitude to date. References: 377 .
1933 - Nation: Russia.
1935 - Nation: USA.
1946 - Nation: USA.
1948 - Nation: USA. Launch Site: White Sands . Launch Complex: LC33. Launch Vehicle: V-2. LV Configuration: V-2 Bumper 2.
First stage failure. V-2 reached 13.4 km, 380 m/s; WAC 13.1 km, 380 m/s.
1951 - Nation: USSR. Launch Vehicle: R-1.
Payload, instruments, left and right animal containers all recovered. Smoke container functioned. Carried dogs. References: 283 , 344 .
1954 - Nation: USA.
AF flight 17. Date estimated. References: 49 , 97 .
1957 - Nation: USA.
Manhigh II reached a record altitude of 101,516 feet (30,950 m) with Major David Simons aboard on 19 and 20 August. Including the pilot and scientific equipment, the total weight of the Manhigh II gondola was 747 kg. At maximum altitude, the ballon expanded to a diameter of 60 m with a volume in excess of 85,000 cubic m.
1959 - Nation: Canada.
1959 - - 19:24 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: LC75-3-5. Launch Vehicle: Thor Agena A. LV Configuration: Thor s/n 200 / Agena A s/n 1028.
KH-1; 1st generation low resolution photo surveillance; film capsule recovery failed. Mission failed. Retro rockets malfunctioned negating recovery. References: 1 , 2 , 5 , 6 .
1960 - Nation: USA. Launch Site: Edwards . Launch Vehicle: X-15A. LV Configuration: X-15 No. 1 Flight 11.
Maximum Speed - 3195 kph. Maximum Altitude - 23159 m. References: 38 , 49 , 97 .
1960 - - 20:38 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Vostok 8K72. LV Configuration: Vostok 8K72 s/n L1-12.
The Soviet Union launched its second unmanned test of the Vostok spacecraft, the Korabl Sputnik II, or Sputnik V. The spacecraft carried two dogs, Strelka and Belka, in addition to a gray rabbit, rats, mice, flies, plants, fungi, microscopic water plants, and seeds. Electrodes attached to the dogs and linked with the spacecraft communications system, which included a television camera, enabled Soviet scientists to check the animals' hearts, blood pressure, breathing, and actions during the trip. After the spacecraft reentered and landed safely the next day, the animals and biological specimens were reported to be in good condition.
Officially: Development of systems ensuring man's life functions and safety in flight and his return to Earth.
References: 1 , 2 , 5 , 6 , 175 .
1962 - Nation: USA.
1963 - Nation: USA. Launch Site: White Sands . Launch Vehicle: Redstone. LV Configuration: Redstone s/n CC-2008.
Successful missile test. Missed aimpoint by 267 m. References: 439 .
1964 - - 12:15 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17A. Launch Vehicle: Delta D. LV Configuration: Thor Delta D s/n 417 / Delta s/n 25.
Experimental commsat; carried Star Flash experiment. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1966 - Nation: USA.
NASA announced selection of McDonnell to manufacture an AM Airlock Module for AAP to permit astronauts to enter the empty hydrogen tank of a spent S-IVB Saturn stage. The AM would form an interstage between the spent rocket stage and the Apollo CSM and would contain environmental and life support systems to make the structure habitable in space. Though MSFC had project responsibility for the complete Orbital Workshop, technical and management responsibility for the AM rested with the AAP office at MSC. Contract negotiations with McDonnell were completed in mid-September. Because design of the AM would employ existing Gemini technology and hardware where feasible, MSC Gemini Deputy Manager Kenneth S. Kleinknecht detailed a number of people from his office to support the AM project.
1966 - Nation: USA. Launch Site: Edwards . Launch Vehicle: X-15A. LV Configuration: X-15 No. 3 Flight 54.
Maximum Speed - 5804 kph. Maximum Altitude - 54250 m. References: 38 , 49 , 97 .
1966 - - 19:26 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC3E. Launch Vehicle: SLV-3 Atlas / Agena D. LV Configuration: Atlas s/n 7202 / Agena D s/n 1352.
Cold welding experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 1 , 2 , 5 , 6 , 278 .
Missile Defense Alarm System. References: 1 , 2 , 5 , 6 , 171 , 172 , 278 .
Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 1 , 2 , 5 , 6 , 278 .
1969 - - 12:57 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Voskhod 11A57.
High resolution photo reconnaissance satellite; returned film capsule References: 1 , 2 , 6 .
1970 - - 12:11 GMT. Nation: UK. Launch Site: Cape Canaveral . Launch Complex: LC17A. Launch Vehicle: Delta M. LV Configuration: Thor Delta M s/n 561 / Delta s/n 80.
AKM failure left in unusable orbit. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1970 - - 15:00 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC133/1. Launch Vehicle: Kosmos 11K63.
1971 - Nation: USSR. Launch Site: Baikonur . Launch Complex: LC31. Launch Vehicle: Voskhod 11A57. FAILURE: Failure.
High resolution photo reconnaissance mission. References: 279 .
1972 - - 02:40 GMT. Nation: Japan. Launch Site: Kagoshima . Launch Complex: M. Launch Vehicle: Mu-3S. LV Configuration: Mu-4S s/n M-4S-4.
Ionospheric experiments. Scientific observations in the ionosphere and magnetosphere. Interjection point 31 deg 15' N 11 deg 05' E. References: 1 , 2 , 5 , 6 .
1982 - - 17:12 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
Docked with Salyut 7. Carried Svetlana Savitskaya, Leonid Popov, Alexander Serebrov to Salyut 7 to conduct scientific and technical research and experiments; returned crew of Soyuz T-5 to Earth. Recovered December 10, 1982 19:03 GMT. Landed 118 km E Dzhezkazgan. References: 1 , 2 , 6 , 32 , 33 , 51 .
1983 - - 06:00 GMT. Nation: China. Launch Site: Jiuquan . Launch Complex: LA2. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C s/n CZ2C-5.
Photo surveillance; film capsule. References: 1 , 2 , 5 , 6 .
1987 - - 07:12 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
Military cartographic satellite; returned film capsule. References: 1 , 2 , 6 .
1992 - - 10:19 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC16/2. Launch Vehicle: Soyuz 11A511U.
Carried US Dept. of Defense experiment. Investigation of the natural resources of the Earth in the interests of the various branches of the national economy and solution of problems relating to the environment and to international cooperation (the satellite's equipment included two Pion passive satellites for the investigation of the upper atmosphere). References: 1 , 2 , 6 .
Deployed from Resurs F16; examined how upper atmosphere affects spacecraft reentries. References: 1 , 2 , 6 .
Deployed from Resurs F16; examined how upper atmosphere affects spacecraft reentries. References: 1 , 2 , 6 .
Geosynchronous. Stationed over 146.0E References: 4 .
1998 - - 23:01 GMT. Nation: USA. Launch Site: Taiyuan . Launch Vehicle: CZ-2C/SD. LV Configuration: Chang Zheng 2C-III/SD no. 19.
Plane 2. Ascending node 199.4 degrees.
Plane 2. Ascending node 199.4 degrees.